Firing Tests and Simulations of a CubeSat-Scale H2O2-Based Hybrid Rocket

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Tests evaluate regression rate and fuel regression in hybrid rockets, indicating design implications for small satellite missions.

Hybrids rocket performance improved with optimized mass flux and regression rate dynamics under varied conditions.
Key metrics reveal efficient propellant combustion and minimal regression rate impact in numerical simulations.
Assessment using computational fluid dynamics models evaluated HDPE performance across multiple test conditions.
Research underscores the need for tailored designs in small-scale hybrid rocket systems for optimal mission effectiveness.

Cassese et al. (2025) studied this question.

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